Hello! At 1:08, when the aircraft "falls" sidewards, does this consider a sideslip? If not, can you make a video on explaining sideslips, dutch roll, phugoid, directional and spiral divergence??
Please explane how the control stick.stick pushed forward makes the flap move up or down?moving the stick to the right makes the makes what flap go yp and what flap go down?thank you for helping me understand
I like the channel and usually agree with what is said. This time however, I am surprised how your logic goes astray: At 0.59 you correctly state that when the plane rolls the LIFT FORCE ROLLS WITH IT, and consequently the remaining lift component pointing in vertical direction is too small to compensate the weight. The consequence is a sideways downwards slide of the plane. Surprisingly, at 2.03 when pitching the plane down or up, the explanation now is that it's the "weight force which contributes to the forward motion and results in increased airspeed". This is utter nonsense. Just look at your graph: The force that gets tilted is still in both cases the lift force. In case of pitching down it is now angled more forward and accelerates the plane. At the same time the vertical force balance - due to the vertical lift component now being reduced - leaves us with a net force downwards (the weight is now bigger than the vertical lift component) and this net force down accelerates the plane also downwards. Together with the forward acceleration the plane is thus accelerated in a downward-forward direction (until it is likely balanced by increasing drag). It is exactly the same mechanism as on the lateral slide, only this time the plane "slides" forward/downwards. If the plane pitches up, the lifting force is angled more backwards. This decellerates the plane horizontally, and still accelerates it vertically as long as the vertical components of lift (and drag, and thrust) are not balancing the weight force. If the force balancing is not resolved in time, the plane will eventually stall and recover its flying speed without the pilot's help🙂
Doing my instructor and these are such a massive help amazing work. Please keep going with this amazing work 😃
Will do. Thank you.
Keep going you guys are revision of my studies
We will. Thank you.
Always posting excellent videos!
Thank you! Cheers!
it was very helpful, loved the explanation, thanks
The secondary effect of the aliroens is adverse yaw not only yaw
Very useful!!! The best I saw on youtube
thank you so much for this really precious information
So nice of you
Hey I found it very helpful thanks for the detailed information with the excellent animation
Keep it up Flight Club 👍👍😁😁
Lovely voice!
I wanna go to colledge for this so bad
Did you? Currently in college for this now and loving it!
Hello! At 1:08, when the aircraft "falls" sidewards, does this consider a sideslip? If not, can you make a video on explaining sideslips, dutch roll, phugoid, directional and spiral divergence??
Most definitely Oscar! We will be tackling these subjects once we've mastered 3D animation. Coming soon!
thanks :DDD
So technically, by rolling you are also losing altitude right?
Can please explain further how elevator affects altitude？ thankss
Please explane how the control stick.stick pushed forward makes the flap
move up or down?moving the stick to the right makes the makes what flap go yp and what flap go down?thank you for helping me understand
Pull=Pitch higher
Push=Pitch lower
I like the channel and usually agree with what is said. This time however, I am surprised how your logic goes astray: At 0.59 you correctly state that when the plane rolls the LIFT FORCE ROLLS WITH IT, and consequently the remaining lift component pointing in vertical direction is too small to compensate the weight. The consequence is a sideways downwards slide of the plane.
Surprisingly, at 2.03 when pitching the plane down or up, the explanation now is that it's the "weight force which contributes to the forward motion and results in increased airspeed". This is utter nonsense. Just look at your graph: The force that gets tilted is still in both cases the lift force.
In case of pitching down it is now angled more forward and accelerates the plane. At the same time the vertical force balance - due to the vertical lift component now being reduced - leaves us with a net force downwards (the weight is now bigger than the vertical lift component) and this net force down accelerates the plane also downwards. Together with the forward acceleration the plane is thus accelerated in a downward-forward direction (until it is likely balanced by increasing drag). It is exactly the same mechanism as on the lateral slide, only this time the plane "slides" forward/downwards.
If the plane pitches up, the lifting force is angled more backwards. This decellerates the plane horizontally, and still accelerates it vertically as long as the vertical components of lift (and drag, and thrust) are not balancing the weight force.
If the force balancing is not resolved in time, the plane will eventually stall and recover its flying speed without the pilot's help🙂